CN204587305U - The electronic unmanned plane of multifunctional foldable eight rotor - Google Patents
The electronic unmanned plane of multifunctional foldable eight rotor Download PDFInfo
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- CN204587305U CN204587305U CN201520139389.8U CN201520139389U CN204587305U CN 204587305 U CN204587305 U CN 204587305U CN 201520139389 U CN201520139389 U CN 201520139389U CN 204587305 U CN204587305 U CN 204587305U
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- cantilever
- plummer
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- rotor
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Abstract
The electronic unmanned plane of multifunctional foldable eight rotor, mainly solves that existing rotor electronic unmanned aerial vehicle purposes is single, the problem of complex structure, complete machine transport difficult.It comprises body, flies control mechanism, actuating unit, foldable cantilever mechanism, spraying mechanism and lithium cell group.Above-mentioned actuating unit comprises electrical motor and screw propeller; Above-mentioned foldable cantilever mechanism comprises cantilever and folding pipe clamp, and its cantilever is arranged on folding pipe clamp, and one end of folding pipe clamp is arranged between downside plummer and upside plummer, other end cantilever mounted.Flying control mechanism is arranged on the plummer of upside; Spraying mechanism is arranged on the below of downside plummer.Cantilever of the present utility model, can regain in transportation, is convenient to complete machine transport, thus reduces traffic cost; Spraying mechanism, can, according to flying speed and the density of spraying target, control to spray flow in real time.It has in aircraft of the same type, and the flight time is long, load-carrying is large, adaptable feature.Can be widely used in that agriculture plant protection is protected, forest fire monitoring, aerophotography, the field such as land survey and consequential loss assessment.
Description
Technical field
The utility model relates to the electronic unmanned plane of a kind of eight rotor, and the electronic unmanned plane of especially a kind of multifunctional foldable eight rotor, belongs to field of aerospace technology.
Background technology
Along with the development of global general-use Aerobiz; the development of various autogiro is also more increasing with day; the particularly electronic unmanned aerial vehicle of rotor; be widely used in the tasks such as agriculture plant protection is protected, forest fire monitoring, aerophotography, land survey, consequential loss assessment; but existing rotor wing unmanned aerial vehicle complex structure, with high costs, be unfavorable for the research-and-development activity of autogiro and the development of General Aviation industry.
Summary of the invention
The utility model is for the purpose of solving the problem, for the deficiencies in the prior art, and a kind of multi-functional, electronic unmanned aerial vehicle of structure simple folding eight rotor is provided, solve that existing rotor electronic unmanned aerial vehicle purposes is single, the problem of complex structure, complete machine transport difficult.
For achieving the above object, the utility model adopts following technical proposals: the electronic unmanned plane of multifunctional foldable eight rotor, comprises body (4).Above-mentioned body (4) comprises alighting gear (6), downside plummer (7) and upside plummer (9), and alighting gear (6) is welded on the below of housing construction (4).Described downside plummer (7) is arranged on body (4), and angle between every two adjacent cantilever is equal.It also comprises and flies control mechanism (3), actuating unit, foldable cantilever mechanism, spraying mechanism (2) and lithium cell group (10).Above-mentioned actuating unit comprises electrical motor (5) and screw propeller (8); Above-mentioned foldable cantilever mechanism comprises cantilever (1) and folding pipe clamp (11), and its cantilever (1) is arranged on folding pipe clamp (11).One end of folding pipe clamp (11) is arranged between downside plummer (7) and upside plummer (9), other end cantilever mounted (1).Above-mentioned electrical motor (5) is arranged on the top of cantilever (1); Flying control mechanism (3) is arranged on upside plummer (9); Spraying mechanism (2) is arranged on the below of downside plummer (7), the both sides of lithium cell group (10), and is fixed on housing construction (4).Above-mentioned lithium cell group (10) is placed on the midway location of the below of downside plummer (7), and is fixed on housing construction (4).
The beneficial effects of the utility model and feature:
(1) foldable cantilever of the present utility model, can regain in transportation, is convenient to complete machine transport, thus reduces traffic cost, reduces the damage to aircraft in complete machine transportation;
(2) spraying mechanism of the present utility model, can according to flying speed and the density of spraying target, flow is sprayed in real-time control, thus can on high efficiency basis, larger is cost-saving, in addition, the appropriate design of spraying mechanism and layout, can make aircraft in operation process, fly more stable, reduce external factor to the impact of flight stability;
(3) there is rational in infrastructure, practical, reliable feature.
The utility model can be widely used in the tasks such as agriculture plant protection is protected, forest fire monitoring, aerophotography, land survey, consequential loss assessment; done optimal design for crop protection (sprinkling) aspect especially, it has in aircraft of the same type, and the flight time is long, load-carrying is large, adaptable feature.
Accompanying drawing explanation
Fig. 1 is front view of the present utility model.
Fig. 2 is the birds-eye view of Fig. 1.
Fig. 3 is the left view of Fig. 1.
Fig. 4 be in Fig. 1 cantilever fold after schematic diagram.
Shown in figure: 1, cantilever; 2, spraying mechanism; 3, control mechanism is flown; 4, body; 5, electrical motor; 6, alighting gear; 7, downside plummer; 8, screw propeller; 9, upside plummer; 10, lithium cell group; 11, folding pipe clamp.
Detailed description of the invention
With reference to Fig. 1-4, the electronic unmanned plane of multifunctional foldable eight rotor, comprises body 4.Above-mentioned body 4 comprises alighting gear 6, downside plummer 7 and upside plummer 9, and alighting gear 6 is welded on the below of housing construction 4.Described downside plummer 7 is arranged on body 4, and angle between every two adjacent cantilever is equal.It also comprises and flies control mechanism 3, actuating unit, foldable cantilever mechanism, spraying mechanism 2 and lithium cell group 10.Above-mentioned actuating unit comprises electrical motor 5 and screw propeller 8; Above-mentioned foldable cantilever mechanism comprises cantilever 1 and folding pipe clamp 11, and its cantilever 1 is arranged on folding pipe clamp 11, and one end of folding pipe clamp 11 is arranged between downside plummer 7 and upside plummer 9, other end cantilever mounted 1.Above-mentioned electrical motor 5 is arranged on the top of cantilever 1; Flying control mechanism 3 is arranged on the plummer 9 of upside; Spraying mechanism 2 is arranged on the below of downside plummer 7, the both sides of lithium cell group 10, and is fixed on housing construction 4.Above-mentioned lithium cell group 10 is placed on the midway location of the below of downside plummer 7, and is fixed on housing construction 4.
Above-mentioned spraying mechanism 2 can be replaced with other equipment according to different job tasks, as: pick up camera, IR sensor, high speed camera etc.
Principle of work of the present utility model: power to electrical motor 5 by lithium cell group 10, thus ensure the normal work of electrical motor 5, and then carrying screws 8 rotates thus provides required lift for aircraft.Controlling the running velocity of electrical motor 5 by flying control mechanism 3, realizing the manipulation to aircraft, controlling spraying mechanism 2 by flying control mechanism 3, thus realize the control to spraying flow.
Claims (3)
1. the electronic unmanned plane of multifunctional foldable eight rotor, comprise body (4), it is characterized in that: described body (4) comprises alighting gear (6), downside plummer (7) and upside plummer (9), alighting gear (6) is welded on the below of housing construction (4), described downside plummer (7) is arranged on body (4), it also comprises and flies control mechanism (3), actuating unit, foldable cantilever mechanism, spraying mechanism (2) and lithium cell group (10), above-mentioned actuating unit comprises electrical motor (5) and screw propeller (8), above-mentioned foldable cantilever mechanism comprises cantilever (1) and folding pipe clamp (11), its cantilever (1) is arranged on folding pipe clamp (11), one end of folding pipe clamp (11) is arranged between downside plummer (7) and upside plummer (9), other end cantilever mounted (1), above-mentioned electrical motor (5) is arranged on the top of cantilever (1), flying control mechanism (3) is arranged on upside plummer (9), spraying mechanism (2) is arranged on the below of downside plummer (7), the both sides of lithium cell group (10), and is fixed on housing construction (4).
2. the electronic unmanned plane of multifunctional foldable eight rotor as claimed in claim 1, is characterized in that: the angle between every two adjacent cantilever (1) is equal.
3. the electronic unmanned plane of multifunctional foldable eight rotor as claimed in claim 1, it is characterized in that: above-mentioned lithium cell group (10) is placed on the midway location of below, downside plummer (7), and is fixed on housing construction (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520139389.8U CN204587305U (en) | 2015-03-10 | 2015-03-10 | The electronic unmanned plane of multifunctional foldable eight rotor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520139389.8U CN204587305U (en) | 2015-03-10 | 2015-03-10 | The electronic unmanned plane of multifunctional foldable eight rotor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204587305U true CN204587305U (en) | 2015-08-26 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520139389.8U Expired - Fee Related CN204587305U (en) | 2015-03-10 | 2015-03-10 | The electronic unmanned plane of multifunctional foldable eight rotor |
Country Status (1)
| Country | Link |
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| CN (1) | CN204587305U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105270618A (en) * | 2015-11-04 | 2016-01-27 | 中航维拓（北京）科技有限责任公司 | Variable-pitch coaxial oil-driven six-rotor helicopter |
| CN105314105A (en) * | 2015-11-13 | 2016-02-10 | 辽宁通用航空研究院 | Hybrid multi-rotor aircraft with retractable wings |
| CN105314101A (en) * | 2015-10-27 | 2016-02-10 | 重庆光煦科技有限公司 | Folding multi-rotor-wing plant protection unmanned plane |
| CN105667760A (en) * | 2016-03-12 | 2016-06-15 | 李遗 | Super-low-altitude remote control flight plant protection machine |
| CN107672799A (en) * | 2017-10-18 | 2018-02-09 | 沈阳旋飞航空技术有限公司 | A kind of electronic unmanned plane |
| US10118697B2 (en) | 2015-06-25 | 2018-11-06 | Riderless Technologies Inc. | Unmanned aerial vehicle |
-
2015
- 2015-03-10 CN CN201520139389.8U patent/CN204587305U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10118697B2 (en) | 2015-06-25 | 2018-11-06 | Riderless Technologies Inc. | Unmanned aerial vehicle |
| CN105314101A (en) * | 2015-10-27 | 2016-02-10 | 重庆光煦科技有限公司 | Folding multi-rotor-wing plant protection unmanned plane |
| CN105270618A (en) * | 2015-11-04 | 2016-01-27 | 中航维拓（北京）科技有限责任公司 | Variable-pitch coaxial oil-driven six-rotor helicopter |
| CN105270618B (en) * | 2015-11-04 | 2017-07-25 | 中航维拓（北京）科技有限责任公司 | A kind of coaxial six heligyro of dynamic displacement of oil |
| CN105314105A (en) * | 2015-11-13 | 2016-02-10 | 辽宁通用航空研究院 | Hybrid multi-rotor aircraft with retractable wings |
| CN105667760A (en) * | 2016-03-12 | 2016-06-15 | 李遗 | Super-low-altitude remote control flight plant protection machine |
| CN107672799A (en) * | 2017-10-18 | 2018-02-09 | 沈阳旋飞航空技术有限公司 | A kind of electronic unmanned plane |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150826 Termination date: 20170310 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |